NASA NTRS · 19800010088
Static pressure orifice system testing method and apparatus
Abstract
A method and apparatus are presented for pressure testing the static pressure orifices and associated connections used in wind tunnels. A cylindrical module, having in one end an open hemispherical calibration pressure chamber separated from and surrounded by an annular vacuum chamber is placed over the orifice of the system to be tested. O-rings ensure seating and a vacuum seal between the chambered end of the module and the surface around the orifice: one O-ring separates the outer chamber from the outside environment. Ports lead from each of the chambers out the other end of the module to tubes connected to a control box consisting of calibration pressure and vacuum supply lines, bleeder valves, and gauges.
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Culotta, R. F., Posey, D. L.. 1980-01-08. Static pressure orifice system testing method and apparatus. https://ntrs.nasa.gov/citations/19800010088
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